Experimental Effects of Scaling on the Performance of Ion Rockets Employing Electron-Bombardment Ion Sources
Overview & Synopsis
A scaling program was undertaken to establish the relations between performance parameters and the size of the electron bombardment ion source. The experimental results of this investigation are the subject of this paper. Two geometrically similar sources, a 5- and a 20-cm-diameter beam source, were scaled from a 10-cm-diameter source to allow a performance comparison to be made. The three ion sources are compared for ion chamber characteristics and overall engine efficiency. The results of the chamber investigations are compared with scaling variations indicated by simple plasma theory. The effects of size on operating limits are also discussed. Mercury was used as the propellant in this investigation.
ntrs.nasa.gov)
Document Information
| Document Title | Experimental Effects of Scaling on the Performance of Ion Rockets Employing Electron-Bombardment Ion Sources |
|---|---|
| Author / Organization | Paul D Reader |
| Subject & Discipline | OTHER |
| Categories | Aerospace & Aviation |
| Publication Year | 1996 |
| License / Rights | Public Domain / NASA STI Open Access |
| Resource Verification | Listed PDF (Verification Pending) |
| Original Host Website |
NASA Technical Reports Server
(ntrs.nasa.gov)
|
| File Format | application/pdf (Portable Document Format) |
| Language | EN |
| Catalog ID | DOC-69004 |
| Original Source Link | Visit Source Page on ntrs.nasa.gov » |